GE CF34-8C1

Service difficulty reports · 1,415

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF348C1'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR N6WA2012072505Warning Message · false activationPAX DOOR OUTER HANDLE CAUTION MESSAGE. PERFORMED OP'S CHECK OF PAX DOOR WARNING SYS IAW AMM 52-70-00. P'S CHECKED GOOD, NO MESSAGE NOTED.Jul 25, 2012 · N355CA · Cndair CL6002C10 · Door Warning SystemSDR N6WA2012072401Lens · delaminatedEXTERIOR EMERGENCY LIGHT LENS AFT OF MAIN PASSENGER DOOR DELAMINATING. R & R LENS IAW AMM 33-51-15.Jul 24, 2012 · N368CA · Cndair CL6002C10 · Emergency LightingSDR N6WA2012072403Lens · delaminatedEXTERIOR EMERGENCY LIGHT LENS AFT OF MAIN PASSENGER DOOR DELAMINATING, R & R LENS IAW AMM 33-51-15.Jul 24, 2012 · N368CA · Cndair CL6002C10 · Emergency LightingSDR ASOA2012072601980Angle · crackedON REMOVAL OF RT LOWER BS 280 WEB FOUND RBL 26 ANGLE CRACKED AT LOWER 2 FASTENER HOLES. REMOVED DAMAGED ANGLE, LOCATED & DRILLED NEW ANGLE, AND INSTALLED IAW SRM 51-42-21-001-001-A01.Jul 23, 2012 · N615QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012072701983Unknown · fumesIN FLT, FUMES DETECTED NEAR GALLEY AREA 1ST CLASS. EMERGENCY DECLARED. DURING INSPECTION, FOUND NO NOTICABLE DEFECTS WITH THE ACFT, NO ODOR OF BURNING PLASTIC WAS FOUND IN GALLEY OR 1ST CLASS. ACFT REMAINS OK FOR SERVICE.Jul 23, 2012 · N753EV · Cndair CL6002C10 · Air Distribution SystemSDR ASOA2012080102012Angle · corrodedTHREE CORRODED L ANGLES BY HINGE INNER CAVITY. REMOVED ANGLES IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLES IAW SRM 51-42-06-001-001-A01.Jul 23, 2012 · N615QX · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2012080902046Floor Skin · crackedLT SIDE OF FWD AVIONIC BAY FLOOR SKIN CRACKED AT FS 193. REPAIRED IAW GREO 670-53-11-509.Jul 23, 2012 · N615QX · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2012080902047Floor Support · corrodedAFT FLOOR SUPPORT CORRODED. REMOVED FROM SUPPORT IAW SRM 51-42-06-001-001-A01. DRILLED NEW AFT FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED FLOOR SUPPORT IAW SRM 51-42-21-001-001, SRM 51-42-06-001-001-A01.Jul 23, 2012 · N615QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR N6WA2012072201Cover · looseEMERGENCY EXIT DOOR COVER LOOSE, RT -PLACED ON NEF RT EMERGENCY EXIT HANDLE COVER CONTROL NR 12406 IAW NEF 25-100-6, CAT 5.Jul 22, 2012 · N367CA · Cndair CL6002C10 · Emergency ExitsSDR ASOA2012072501969Bulb · burned outFWD FUSELAGE, EMERGENCY LIGHTS INOPERATIVE. R & R TWO FWD LIGHT ASSY BULBS. PERFORMED OPS TEST IAW AMM 33-51-15-710-801. OPS CHECKED GOOD.Jul 19, 2012 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012072601978Seat Track · corroded9L SEAT TRACK SECTION FROM FS 830-969 HAS CORROSION. REMOVED CORROSION IAW 53-51-49-101-001-A01. PERFORMED LPI TYPE 1, METHOD-C ON BLEND AREAS IAW SRM 53-51-49-101-001-A01 MAC NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED.Jul 19, 2012 · N615QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012072601979Seat Track · corroded9R SEAT TRACK SECTION HAS CORROSION AT 724. REMOVED CORROSION IAW SRM 53-41-49-101-001-A01. REMOVED .014 FROM TOP (U) LIMIT .035 .021 REMAINING. REMOVED .012 FROM CENTER (T) LIMIT .035 023 REMAINING. PERFORMED LPI, TYPE 1, METHOD-C ON BLEND AREA IAW SRM 5Jul 19, 2012 · N615QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080902044Seat Track · corroded9R SEAT TRACK SECTION FROM FS 349-485 HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801.Jul 19, 2012 · N615QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012072601976Seat Track · corrodedSEAT TRACK CORRODED AT 9L AND FS 601, 613, 629, 665. REMOVED CORROSION IAW SRM 53-31-49-101-001-A01. PERFORMED LPI, TYPE 1, METHOD-C ON BLENDED AREAS IAW SRM 53-31-49-101-001A-01 IAW NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED.Jul 18, 2012 · N615QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012072601977Seat Track · corroded9R SEAT TRACK SECTION FROM FS 830-969 HAS CORROSION AND GOUGED. REMOVED CORROSION IAW SRM 53-51-49-101-001-A01. PERFORMED LPI TYPE 1 METHOD-C ON BLEND AREA IAW SRM 53-51-49-101-001-A01 IAW MAC NDT INSPECTION PROCEDURE PT-1, NO INDICATIONS NOTED.Jul 18, 2012 · N615QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102011Seat Track · corrodedSEAT TRACK CORRODED AT 9L FWD SECTION AT FWD END FS 364 AND 379, 420, 469, 485. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01. INSTALLED NEW SERVICEABLE TRACK IAW AMM 53-00-49-40Jul 18, 2012 · N615QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR CA120719009Unknown · smoke(CAN) DURING DECENT FLIGHT CREW SMELLED WOOD ODOR IN COCKPIT. F/A AND PASSENGERS REPORTED SEEING SMOKE WITH ELECTRICAL ODOR IN CABIN. BOTH OVERWING EMERGENCY EXITS OPENED.Jul 18, 2012 · Cndair CL6002C10 · Air Distribution SystemSDR ASOA2012071901943Frame · corrodedCORROSION ON FS 349 FRAME FROM STRINGERS 24-26 RIGHT.Jul 16, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012072601973Door · no testLEFT EMERGENCY EXIT FAILED FUNCTIONAL TEST, REQUIRES 78LBS OF FORCE. CLEANED AND LUBED EMERGENCY EXIT IAW AMM 12-20-52-640-802. PERFORMED FUNCTIONAL CHECK IAW AMM 52-21-00-720-801, CHECKED GOOD .Jul 16, 2012 · N615QX · Cndair CL6002C10 · Emergency ExitsSDR ASOA2012072601974Door · no testRIGHT EMERGENCY EXIT FAILED FUNCTIONAL TEST, REQUIRES 64LBS OF FORCE. CLEANED AND LUBED RT EMERGENCY EXIT IAW AMM 12-20-52-641-802. FUNCTIONAL CHECKED IAW AMM 52-21-00-720-801.Jul 16, 2012 · N615QX · Cndair CL6002C10 · Emergency ExitsSDR ASOA2012072601975Door · out of adjustFORCE TO COMPLETE THE UNLATCH CYCLE FOR THE FORWARD GALLEY SERVICE DOOR EXCEEDS ALLOWABLE LIMITS. ADJUSTED LATCH MECHANISM TO ALLOWABLE LIMITS IAW AMM 52-41-02-820-801-A01. FUNCTIONAL TEST OF THE GALLEY SERVICE DOOR COMPLY WITH IAW AMM CH 25-41-00-720-802.Jul 16, 2012 · N615QX · Cndair CL6002C10 · Service DoorsSDR ASOA2012080902042Web · corrodedLEFT BS 280 WEB CORRODED. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW GREO 670-53-11-0594.Jul 16, 2012 · N615QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071801918Stringer Splice · corrodedSTRINGER SPLICE 26R FS 333, FOUND CORRODED OUT OF LIMITS. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001.Jul 13, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801919Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 295 & 310.Jul 13, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801920Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 349-364.Jul 13, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801921Intercostal · corrodedCORROSION AT FS 364 INTERCOSTAL BETWEEN STRINGERS 26 & 27L.Jul 13, 2012 · N740EV · Cndair CL2151A10 · Fuselage Miscellaneous StructureSDR ASOA2012071901941Intercostal · corrodedCORROSION AT FS 364 RT INTERCOSTAL BETWEEN STRINGERS 27 & 26R. INSTALLED INTERCOSTAL AT FS 364 RT INTERCOSTAL IAW SRM 51-42-21-001-001.Jul 13, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012072401965Windshield · failedLEFT WINDOW AND LT WINDSHIELD CAUTION MESSAGE FOLLOWED BY SPARKS AND A PUFF OF SMOKE FROM LOWER LT WINDSHIELD CONTROLLER. R & R LT WINDSHIELD IAW AMM 56-11--01. OPS CHECKED GOOD.Jul 12, 2012 · N760EV · Cndair CL6002C10 · Flight Compartment WindowsSDR ASOA2012071301901Socket · brokenPAX DOOR FLOOR EMERGENCY FLOODLIGHT HAS MISSING COVER AND BROKEN LIGHT SOCKET. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-11. OPS CHECK GOOD. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-11. OPS CHECK GOOD. SDR CJul 10, 2012 · N755EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012071901939Frame · corrodedCORROSION ON FS 349 FRAME FROM STRINGERS 24-26 RIGHT. BLENDED CORROSION AND FOUND FRAME TO BE OUT OF LIMITS REF SRM 51-21-06-001-001 & SRM 53-21-06-101-006. REMOVED FRAME IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED AND DRILLED NEW FRAMEJul 9, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012071901940Stringer · corrodedCORROSION ON STRINGER 25 RIGHT FROM FS 349 - 333. REMOVED CORROSION ON STRINGER AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED STRINGER 25R IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED & DRILLED NEW STRINGER IAW SRM 51-Jul 9, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071301893Sill · corrodedAFT CARGO DOOR SILL CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01.Jul 6, 2012 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071301892Stringer · corrodedAVIONICS COMPARTMENT, STRINGER 26R IS CORRODED BETWEEN BS 333-349. REMOVED AND REPLACED STRINGER IAW SRM 51-42-06-001-001-A01.Jul 5, 2012 · N744EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071901938Floor Support · corrodedLT AFT CARGO FLOOR SUPPORT UNDER PANEL 281JLF HAS SURFACE CORROSION BETWEEN FS 1015 TO 1045. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. MEASURED AREA, ORIGINAL MATERIAL THICKNESS .063" BLEND DIMENSIONS : 5.3"X2.1X.035", .028" REMAINING; 2.7" X 1.4"X .005",Jul 5, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071901937Sill · crackedFWD EQUIPMENT COMPARTMENT RT SIDE, SILL UNDER THE ADG HYD PUMP IS CRACKED. REPAIRED IAW GREO 670-53-11-504 AND ECTC REO 670-53-11-509.Jul 3, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012070901868Light · brokenLIGHT, AISLE WITH ARROW BROKEN AT END OF TRACK. RECEIVED NEW TRACK LIGHTING SEGMENT,Jul 2, 2012 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012071801912Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 295 AND 310. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-21-03-101-003-A01. REMOVED STRINGER REF SRM 51-42-06-001-001. DRILLED NEW SECTION OF STRINGER 26R REF SRM 51-40-11-001-001.Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801913Channel · corrodedCHANNEL CORRODED AT FS 305 AND S27 ABOVE ANTENNA. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01-101-002-A01. R & R CHANNEL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071801914Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 349 TO 364. CORROSION FOUND OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED STRINGER SPLICE AND SECTION OF STRINGER IAW SRM 51-42-06-001-001. DRILLED NEW SECTION OF STRINGER IAW SRM 51-40-11-001-001. INSTALLED STRIJul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801915Intercostal · corrodedCORROSION AT FS 364 INTERCOSTAL BETWEEN STRINGERS 27 AND 26L. BLENDED CORROSSION AND FOUND OUT OF LIMITS REF SRM 53-21-23-101-003-A01 & SRM 51-21-06-001-001. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001 & SRM 51-42-21-001-001. INSTALLED NEW INTERCOSTAL IAJul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071801916Stringer · corrodedCORROSION AT FS 364 STRINGER 26L. CORROSION OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01. DRILLED NEW STRINGER AND INSTALLED IAW SRM 51-42-06-001-001.Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071901935Intercostal · corrodedCORROSION AT FS 364 RT INTERCOSTAL BETWEEM STRG27 AND 26R. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06-001-001-A01.Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071901936Frame · corrodedCORROSION AT FS 333 BETWEEN STRINGERS 26 AND 27 LEFT. BLENDED DAMAGE ON FRAME. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .040" ORIGINAL IS .050" MATERIAL REMOVED IS .010" . REPAIRED IAW REO 670-Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012072501967Support · corrodedCORROSION ON NLG NOSE JACK FITTING SUPPORTS (LT AND RT) BETWEEN FS 265.00 AND FS 280.00. BLEND DAMAGE FROM FITTING SUPPORTS DETERMINE REMAINING MATERIAL & SUBMIT TO THD REF SRM 51-21-06-001-001. STARTED BLENDING LT AND RT SIDE OF NOSE JACK SUPPORT FITTING IAJul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012072501968Frame · corrodedCORROSION ON FRAME AT FS 319 AND FROM STRINGERS 26L TO 26R. REMOVED CORROSION ON FRAME IAW SRM 53-21-06-101-002-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .042"7, ORIGINAL IS .050" MJul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR N6WA2012070101Placard · peelingEXIT PLACARD PEELING OFF OF MAIN CABIN DOOR STAIR. PLACED ON NEF 25-500-1, CAT 5.Jul 1, 2012 · N376CA · Cndair CL6002C10 · Placards and MarkingsSDR ASOA2012070301859Door · bindingF/A REPORTS DIFFICULTY OPENING MAIN PAX DOOR. LEVER HANGS UP WHEN OPERATING. PERFORMED A CLEANING, INSPECTION, & OPS CHECK OF THE PASSENGER DOOR IAW AMM 52-11-00. INSPECTED & OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED, ACFT OK FOR SERVICE.Jul 1, 2012 · N604QX · Cndair CL6002C10 · Passenger/Crew DoorsSDR N6WA2012062802Actuator · failedPITCH FEEL CAUTION IN FLIGHT. R & R NR 2 PITCH FEEL ACTUATOR IAW AMM 27-31-23.Jun 28, 2012 · N379CA · Cndair CL6002C10 · Elevator Control SystemSDR ASOA2012070901870Sill · corrodedPAX DOOR SILL IS CORRODED ON FORWARD SIDE. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED SILL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.Jun 26, 2012 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012070901871Floor Support · corrodedFLOOR SUPPORT AT PAX DOOR IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED FLOOR SUPPORTAW SRM 51-41-02-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-41-02-001-001-A01.Jun 26, 2012 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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